#1. The landing reference speed V ref has, in accordance with international requirements, the following margins above the stall speed in landing configuration for a Class B aeroplane:
#2. At a given mass, the stalling speed of a twin engine, class B aeroplane is 100kt in the landing configuration. The minimum speed a pilot must maintain in short final is:
#3. The stalling speed or the minimum steady flight speed at which the aeroplane is controllable in landing configuration is abbreviated as:
#4. What margin above the stall speed is provided by the landing reference V ref for a Class B aeroplane?
#5. An increase in atmospheric pressure has, among other things, the following consequences on landing performance:
#6. The take-off distance of an aircraft is 600 m in a standard atmosphere, with no wind and at a pressure altitude of 0 ft. Using the following corrections: ± 20m / 1,000 ft field elevation, - 5m /kt headwind, ± 15m / % runway slope, ± 5m /°C deviation from standard temperature. The take-off distance from an airport at 1,000 ft elevation, temperature 17°C, QNH 1013.25 hPa, 1% up-slope, 10 kt tailwind is?
#7. To minimize the risk of hydroplaning during the landing the pilot of a modern airliner should:
#8. An aircraft has two certified landing flaps positions 25° and 35°. If a pilot chooses 25° instead of 35°, the aircraft will have:
#9. May anti-skid be considered to determine the take-off and landing data?
#10. An aircraft has two certified landing flaps positions, 25° and 35°. If a pilot chooses 35° instead of 25°, the aircraft will have: